Dynamic UAV Transport Tasks

ABSTRACT

Example implementations relate to a method of dynamically updating a transport task of a UAV. The method includes receiving, at a transport-provider computing system, an item provider request for transportation of a plurality of packages from a loading location at a given future time. The method also includes assigning, by the transport-provider computing system, a respective transport task to each of a plurality of UAVs, where the respective transport task comprises an instruction to deploy to the loading location to pick up one or more of the plurality of packages. Further, the method includes identifying, by the transport-provider system, a first package while or after a first UAV picks up the first package. Yet further, the method includes based on the identifying of the first package, providing, by the transport-provider system, a task update to the first UAV to update the respective transport task of the first UAV.

BACKGROUND

An unmanned system, which may also be referred to as an autonomousvehicle, is a vehicle capable of travel without a physically-presenthuman operator. An unmanned system may operate in a remote-control mode,in an autonomous mode, or in a partially autonomous mode.

When an unmanned system operates in a remote-control mode, a pilot ordriver that is at a remote location can control the unmanned vehicle viacommands that are sent to the unmanned vehicle via a wireless link. Whenthe unmanned system operates in autonomous mode, the unmanned systemtypically moves based on pre-programmed navigation waypoints, dynamicautomation systems, or a combination of these. Further, some unmannedsystems can operate in both a remote-control mode and an autonomousmode, and in some instances may do so simultaneously. For instance, aremote pilot or driver may wish to leave navigation to an autonomoussystem while manually performing another task, such as operating amechanical system for picking up objects, as an example.

Various types of unmanned systems exist for various differentenvironments. For instance, unmanned aerial vehicles (UAVs) areconfigured for operation in the air (e.g., flight). Examples includequad-copters and tail-sitter UAVs, among others. Unmanned systems alsoexist for hybrid operations in which multi-environment operation ispossible. Examples of hybrid unmanned vehicles include an amphibiouscraft that is capable of operation on land as well as on water or afloatplane that is capable of landing on water as well as on land. Otherexamples are also possible.

Such unmanned systems can be used by an aerial transport serviceprovider (ATSP) to transport items. In practice, to providetransportation services to an item provider, an ATSP can deploy to aloading location a plurality of UAVs, each of which is assigned aspecific package to pick up and deliver. As such, when each UAV arrivesat the loading location, the item provider can identify the UAV in orderto determine the packages that are assigned to the UAV. Then, the itemprovider can load into a payload compartment of the UAV the packagesthat are assigned to the UAV.

However, this process of loading a package into a payload compartmentcan take an unsatisfactorily long period of time, thereby hindering theefficiency and speed of the delivery. Particularly, the item providermust perform several steps when a UAV arrives at the loading location.For instance, the item provider must identify the UAV, determine thepackage that is assigned to the UAV, locate the package, and load thepackage into a payload compartment of the UAV. As the item providerperforms these steps, the UAV is merely idling, and therefore, iswasting limited resources such as time and UAV battery power.Squandering such resources can negatively impact the speed, timeliness,and reliability of the transportation service provided by the ATSP.Additionally, these problems with the loading process are furtherexpounded as the number of packages that the item provider wants todeliver increases.

SUMMARY

An aerial transport service provider (ATSP) can use a fleet of UAVs toprovide entities with transportation services. In practice, to transportpackages, the ATSP assigns each of the UAVs in the fleet a package topick up from the entity. However, when a UAV picks up its assignedpackage, locating and loading the package can take a lengthy period oftime, during which the UAV is idling, thereby wasting resources (e.g.,time and UAV battery power). Squandering such resources can negativelyimpact the reliability and speed of the transportation service.Accordingly, example embodiments may help streamline the package pick-upprocess by dynamically updating a transport task of a UAV based on apackage that is loaded into a payload compartment of the UAV. Inparticular, rather than assigning a UAV a specific package to pick up,the ATSP can generate a transport task for the UAV to pick up a packageat random from the packages that are ready for delivery. Once thepackage is picked up, the package can be identified, and based on theidentity of the package, the ATSP can dynamically update the transporttask of the UAV to provide the UAV with a route to the package'sdelivery location.

In one aspect, a method is disclosed. The method includes receiving, ata transport-provider computing system, an item provider request fortransportation of a plurality of packages from a loading location at agiven future time. The method also includes the assigning, by thetransport-provider computing system, a respective transport task to eachof a plurality of unmanned aerial vehicles (UAV), wherein the respectivetransport task comprises an instruction to deploy to the loadinglocation to pick up one or more of the plurality of packages. Further,the method includes, identifying, by the transport-provider computingsystem, a first package while or after a first UAV of the plurality ofUAVs picks up the first package. Yet further, the method includes basedon the identifying of the first package, providing, by thetransport-provider computing system, a task update to the first UAV toupdate the respective transport task of the first UAV.

In another aspect, a UAV is disclosed. The UAV includes a payloadcompartment operable to hold one or more packages, and a packageidentification device arranged in an interior of the payloadcompartment, where the package identification device is configured toidentify the one or more packages held in the payload compartment. TheUAV also includes a computer apparatus having one or more processors andmemory storing instructions that, when executed by the one or moreprocessors, cause the system to carry out operations including:receiving, from a transport-provider computing system, a transport taskindicating an instruction to fly to a loading location to pick up apackage from a plurality of packages located at the loading location;causing the UAV to fly to the loading location; at the loading location,causing the UAV to pick up a first package from the plurality ofpackages; causing the package identification device to scan, sense orotherwise interact with a unique identifier of the first package;communicating the unique identifier to the transport-provider computingsystem; and in response, receiving a task update from thetransport-provider computing system.

In yet another aspect, a method is disclosed. The method includesreceiving, from a transport-provider computing system, a transport taskindicating an instruction to fly to a loading location to pick up apackage from a plurality of packages located at the loading location;causing the UAV to fly to the loading location; at the loading location,causing the UAV to pick up a first package from the plurality ofpackages; causing the package identification device to scan, sense orotherwise interact with a unique identifier of the first package;communicating the unique identifier to the transport-provider computingsystem; and in response, receiving a task update from thetransport-provider computing system.

In yet another aspect, a non-transitory computer-readable medium isdisclosed. The non-transitory computer-readable medium has storedthereon program instructions that when executed by the processor causethe computing device to perform a set of functions including: receivingan item provider request for transportation of a plurality of packagesfrom a loading location at a given future time; assigning a respectivetransport task to each of a plurality of unmanned aerial vehicles (UAV),wherein the respective transport task comprises an instruction to deployto the loading location to pick up one or more of the plurality ofpackages; identifying a first package while or after a first UAV of theplurality of UAVs picks up the first package; and based on theidentifying of the first package, providing a task update to the firstUAV to update the respective transport task of the first UAV.

In yet another aspect, a system is disclosed. The system includes meansfor: receiving an item provider request for transportation of aplurality of packages from a loading location at a given future time;assigning a respective transport task to each of a plurality of unmannedaerial vehicles (UAV), wherein the respective transport task comprisesan instruction to deploy to the loading location to pick up one or moreof the plurality of packages; identifying a first package while or aftera first UAV of the plurality of UAVs picks up the first package; andbased on the identifying of the first package, providing a task updateto the first UAV to update the respective transport task of the firstUAV.

These as well as other aspects, advantages, and alternatives, willbecome apparent to those of ordinary skill in the art by reading thefollowing detailed description, with reference where appropriate to theaccompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A is a simplified illustration of an unmanned aerial vehicle,according to example embodiments.

FIG. 1B is a simplified illustration of an unmanned aerial vehicle,according to example embodiments.

FIG. 1C is a simplified illustration of an unmanned aerial vehicle,according to example embodiments.

FIG. 1D is a simplified illustration of an unmanned aerial vehicle,according to example embodiments.

FIG. 1E is a simplified illustration of an unmanned aerial vehicle,according to example embodiments.

FIG. 2 is a simplified block diagram illustrating components of anunmanned aerial system, according to example embodiments.

FIG. 3 is a simplified block diagram illustrating a distributed UAVsystem, according to example embodiments.

FIG. 4 is a block diagram showing an example arrangement for a transportprovider system, according to example implementations.

FIGS. 5A and 5B are simplified illustrations of an unmanned aerialvehicle having a scanning device installed in a payload compartment,according to example implementations.

FIG. 6 is a simplified illustration of a package being placed into apayload compartment of an unmanned aerial vehicle, according to exampleimplementations.

FIGS. 7A and 7B each illustrate a fleet of unmanned aerial vehiclespicking up packages, according to example implementations.

FIG. 8 is a flowchart of a method, according to example implementations.

FIG. 9 is a flowchart of another method, according to exampleimplementations.

DETAILED DESCRIPTION

Example methods and systems are described herein. It should beunderstood that the words “example” and “example” are used herein tomean “serving as an example, instance, or illustration.” Any embodimentor feature described herein as being an “example” or “example” is notnecessarily to be construed as preferred or advantageous over otherembodiments or features. The example embodiments described herein arenot meant to be limiting. It will be readily understood that certainaspects of the disclosed systems and methods can be arranged andcombined in a wide variety of different configurations, all of which arecontemplated herein.

Furthermore, the particular arrangements shown in the Figures should notbe viewed as limiting. It should be understood that other embodimentsmight include more or less of each element shown in a given Figure.Further, some of the illustrated elements may be combined or omitted.Yet further, an example embodiment may include elements that are notillustrated in the Figures.

I. OVERVIEW

In some cases, an ATSP can be a separate entity from an entity orentities that provide items for transportation and/or interface withrecipients who request delivery of the items. In these cases, the itemprovider could request transportation services when one or more packages(that each includes one or more items) are ready to be transported froma loading location, such as a warehouse operated by or affiliated withthe item provider. Additionally and or alternatively, the item providercould have an agreement with the ATSP in which transportation servicesare provided at a scheduled date and/or time.

To overcome at least the problems described above with the loadingprocess, disclosed herein are methods of dynamically updating atransport task of a UAV that is delivering a package. In an embodiment,in response to receiving a transport request from an item provider, theATSP can assign each of one or more UAVs a respective transport task,where the respective transport task instructs the UAV to fly to theloading location and to pick up a package at random, in a predeterminedorder or sequence, or otherwise without specific package assignment,from the packages that are ready for delivery. Once a UAV picks up apackage, the package can be identified, perhaps by using a deviceinstalled within the payload compartment of the UAV. Based on theidentity of the package, the ATSP can determine a delivery location ofthe package, and can send the UAV a task update that specifies at leastthe delivery location of the package.

Accordingly, as opposed to assigning each UAV one or more specificpackages to pick up, the ATSP can deploy UAVs to pick up packages atrandom, in a predetermined order or sequence, or otherwise withoutspecific package assignment, from the loading location, and then candynamically update the transport task of each UAV based on the packagethat the UAV picks up. By doing so, the ATSP can eliminate the need foran extensive loading process, thereby conserving resources such as timeand UAV battery power, which in turn, increases the efficiency and speedof the transport service.

II. ILLUSTRATIVE UNMANNED VEHICLES

Herein, the terms “unmanned aerial system” and “UAV” refer to anyautonomous or semi-autonomous vehicle that is capable of performing somefunctions without a physically present human pilot.

A UAV can take various forms. For example, a UAV may take the form of afixed-wing aircraft, a glider aircraft, a tail-sitter aircraft, a jetaircraft, a ducted fan aircraft, a lighter-than-air dirigible such as ablimp or steerable balloon, a rotorcraft such as a helicopter ormulticopter, and/or an ornithopter, among other possibilities. Further,the terms “drone,” “unmanned aerial vehicle system” (UAVS), or “unmannedaerial vehicle” (UAV) may also be used to refer to a UAV.

FIG. 1A is an isometric view of an example UAV 100. UAV 100 includeswing 102, booms 104, and a fuselage 106. Wings 102 may be stationary andmay generate lift based on the wing shape and the UAV's forwardairspeed. For instance, the two wings 102 may have an airfoil-shapedcross section to produce an aerodynamic force on UAV 100. In someembodiments, wing 102 may carry horizontal propulsion units 108, andbooms 104 may carry vertical propulsion units 110. In operation, powerfor the propulsion units may be provided from a battery compartment 112of fuselage 106. In some embodiments, fuselage 106 also includes anavionics compartment 114, an additional battery compartment (not shown)and/or a delivery unit (not shown, e.g., a winch system) for handlingthe payload. In some embodiments, fuselage 106 is modular, and two ormore compartments (e.g., battery compartment 112, avionics compartment114, other payload and delivery compartments) are detachable from eachother and securable to each other (e.g., mechanically, magnetically, orotherwise) to contiguously form at least a portion of fuselage 106.

In some embodiments, booms 104 terminate in rudders 116 for improved yawcontrol of UAV 100. Further, wings 102 may terminate in wing tips 117for improved control of lift of the UAV.

In the illustrated configuration, UAV 100 includes a structural frame.The structural frame may be referred to as a “structural H-frame” or an“H-frame” (not shown) of the UAV. The H-frame may include, within wings102, a wing spar (not shown) and, within booms 104, boom carriers (notshown). In some embodiments the wing spar and the boom carriers may bemade of carbon fiber, hard plastic, aluminum, light metal alloys, orother materials. The wing spar and the boom carriers may be connectedwith clamps. The wing spar may include pre-drilled holes for horizontalpropulsion units 108, and the boom carriers may include pre-drilledholes for vertical propulsion units 110.

In some embodiments, fuselage 106 may be removably attached to theH-frame (e.g., attached to the wing spar by clamps, configured withgrooves, protrusions or other features to mate with correspondingH-frame features, etc.). In other embodiments, fuselage 106 similarlymay be removably attached to wings 102. The removable attachment offuselage 106 may improve quality and or modularity of UAV 100. Forexample, electrical/mechanical components and/or subsystems of fuselage106 may be tested separately from, and before being attached to, theH-frame. Similarly, printed circuit boards (PCBs) 118 may be testedseparately from, and before being attached to, the boom carriers,therefore eliminating defective parts/subassemblies prior to completingthe UAV. For example, components of fuselage 106 (e.g., avionics,battery unit, delivery units, an additional battery compartment, etc.)may be electrically tested before fuselage 106 is mounted to theH-frame. Furthermore, the motors and the electronics of PCBs 118 mayalso be electrically tested before the final assembly. Generally, theidentification of the defective parts and subassemblies early in theassembly process lowers the overall cost and lead time of the UAV.Furthermore, different types/models of fuselage 106 may be attached tothe H-frame, therefore improving the modularity of the design. Suchmodularity allows these various parts of UAV 100 to be upgraded withouta substantial overhaul to the manufacturing process.

In some embodiments, a wing shell and boom shells may be attached to theH-frame by adhesive elements (e.g., adhesive tape, double-sided adhesivetape, glue, etc.). Therefore, multiple shells may be attached to theH-frame instead of having a monolithic body sprayed onto the H-frame. Insome embodiments, the presence of the multiple shells reduces thestresses induced by the coefficient of thermal expansion of thestructural frame of the UAV. As a result, the UAV may have betterdimensional accuracy and/or improved reliability.

Moreover, in at least some embodiments, the same H-frame may be usedwith the wing shell and/or boom shells having different size and/ordesign, therefore improving the modularity and versatility of the UAVdesigns. The wing shell and/or the boom shells may be made of relativelylight polymers (e.g., closed cell foam) covered by the harder, butrelatively thin, plastic skins.

The power and/or control signals from fuselage 106 may be routed to PCBs118 through cables running through fuselage 106, wings 102, and booms104. In the illustrated embodiment, UAV 100 has four PCBs, but othernumbers of PCBs are also possible. For example, UAV 100 may include twoPCBs, one per the boom. The PCBs carry electronic components 119including, for example, power converters, controllers, memory, passivecomponents, etc. In operation, propulsion units 108 and 110 of UAV 100are electrically connected to the PCBs.

Many variations on the illustrated UAV are possible. For instance,fixed-wing UAVs may include more or fewer rotor units (vertical orhorizontal), and/or may utilize a ducted fan or multiple ducted fans forpropulsion. Further, UAVs with more wings (e.g., an “x-wing”configuration with four wings), are also possible. Although FIG. 1illustrates two wings 102, two booms 104, two horizontal propulsionunits 108, and six vertical propulsion units 110 per boom 104, it shouldbe appreciated that other variants of UAV 100 may be implemented withmore or less of these components. For example, UAV 100 may include fourwings 102, four booms 104, and more or less propulsion units (horizontalor vertical).

FIG. 1A is an isometric view of an example UAV 100. UAV 100 includeswing 102, booms 104, and a fuselage 106. Wings 102 may be stationary andmay generate lift based on the wing shape and the UAV's forwardairspeed. For instance, the two wings 102 may have an airfoil-shapedcross section to produce an aerodynamic force on UAV 100. In someembodiments, wing 102 may carry horizontal propulsion units 108, andbooms 104 may carry vertical propulsion units 110. In operation, powerfor the propulsion units may be provided from a battery compartment 112of fuselage 106. In some embodiments, fuselage 106 also includes anavionics compartment 114, an additional battery compartment (not shown)and/or a delivery unit (not shown, e.g., a winch system) for handlingthe payload. In some embodiments, fuselage 106 is modular, and two ormore compartments (e.g., battery compartment 112, avionics compartment114, other payload and delivery compartments) are detachable from eachother and securable to each other (e.g., mechanically, magnetically, orotherwise) to contiguously form at least a portion of fuselage 106.

In some embodiments, booms 104 terminate in rudders 116 for improved yawcontrol of UAV 100. Further, wings 102 may terminate in wing tips 117for improved control of lift of the UAV.

In the illustrated configuration, UAV 100 includes a structural frame.The structural frame may be referred to as a “structural H-frame” or an“H-frame” (not shown) of the UAV. The H-frame may include, within wings102, a wing spar (not shown) and, within booms 104, boom carriers (notshown). In some embodiments the wing spar and the boom carriers may bemade of carbon fiber, hard plastic, aluminum, light metal alloys, orother materials. The wing spar and the boom carriers may be connectedwith clamps. The wing spar may include pre-drilled holes for horizontalpropulsion units 108, and the boom carriers may include pre-drilledholes for vertical propulsion units 110.

In some embodiments, fuselage 106 may be removably attached to theH-frame (e.g., attached to the wing spar by clamps, configured withgrooves, protrusions or other features to mate with correspondingH-frame features, etc.). In other embodiments, fuselage 106 similarlymay be removably attached to wings 102. The removable attachment offuselage 106 may improve quality and or modularity of UAV 100. Forexample, electrical/mechanical components and/or subsystems of fuselage106 may be tested separately from, and before being attached to, theH-frame. Similarly, printed circuit boards (PCBs) 118 may be testedseparately from, and before being attached to, the boom carriers,therefore eliminating defective parts/subassemblies prior to completingthe UAV. For example, components of fuselage 106 (e.g., avionics,battery unit, delivery units, an additional battery compartment, etc.)may be electrically tested before fuselage 106 is mounted to theH-frame. Furthermore, the motors and the electronics of PCBs 118 mayalso be electrically tested before the final assembly. Generally, theidentification of the defective parts and subassemblies early in theassembly process lowers the overall cost and lead time of the UAV.Furthermore, different types/models of fuselage 106 may be attached tothe H-frame, therefore improving the modularity of the design. Suchmodularity allows these various parts of UAV 100 to be upgraded withouta substantial overhaul to the manufacturing process.

In some embodiments, a wing shell and boom shells may be attached to theH-frame by adhesive elements (e.g., adhesive tape, double-sided adhesivetape, glue, etc.). Therefore, multiple shells may be attached to theH-frame instead of having a monolithic body sprayed onto the H-frame. Insome embodiments, the presence of the multiple shells reduces thestresses induced by the coefficient of thermal expansion of thestructural frame of the UAV. As a result, the UAV may have betterdimensional accuracy and/or improved reliability.

Moreover, in at least some embodiments, the same H-frame may be usedwith the wing shell and/or boom shells having different size and/ordesign, therefore improving the modularity and versatility of the UAVdesigns. The wing shell and/or the boom shells may be made of relativelylight polymers (e.g., closed cell foam) covered by the harder, butrelatively thin, plastic skins.

The power and/or control signals from fuselage 106 may be routed to PCBs118 through cables running through fuselage 106, wings 102, and booms104. In the illustrated embodiment, UAV 100 has four PCBs, but othernumbers of PCBs are also possible. For example, UAV 100 may include twoPCBs, one per the boom. The PCBs carry electronic components 119including, for example, power converters, controllers, memory, passivecomponents, etc. In operation, propulsion units 108 and 110 of UAV 100are electrically connected to the PCBs.

Many variations on the illustrated UAV are possible. For instance,fixed-wing UAVs may include more or fewer rotor units (vertical orhorizontal), and/or may utilize a ducted fan or multiple ducted fans forpropulsion. Further, UAVs with more wings (e.g., an “x-wing”configuration with four wings), are also possible. Although FIG. 1illustrates two wings 102, two booms 104, two horizontal propulsionunits 108, and six vertical propulsion units 110 per boom 104, it shouldbe appreciated that other variants of UAV 100 may be implemented withmore or less of these components. For example, UAV 100 may include fourwings 102, four booms 104, and more or less propulsion units (horizontalor vertical).

Similarly, FIG. 1B shows another example of a fixed-wing UAV 120. Thefixed-wing UAV 120 includes a fuselage 122, two wings 124 with anairfoil-shaped cross section to provide lift for the UAV 120, a verticalstabilizer 126 (or fin) to stabilize the plane's yaw (turn left orright), a horizontal stabilizer 128 (also referred to as an elevator ortailplane) to stabilize pitch (tilt up or down), landing gear 130, and apropulsion unit 132, which can include a motor, shaft, and propeller.

FIG. 1C shows an example of a UAV 140 with a propeller in a pusherconfiguration. The term “pusher” refers to the fact that a propulsionunit 142 is mounted at the back of the UAV and “pushes” the vehicleforward, in contrast to the propulsion unit being mounted at the frontof the UAV. Similar to the description provided for FIGS. 1A and 1B,FIG. 1C depicts common structures used in a pusher plane, including afuselage 144, two wings 146, vertical stabilizers 148, and thepropulsion unit 142, which can include a motor, shaft, and propeller.

FIG. 1D shows an example of a tail-sitter UAV 160. In the illustratedexample, the tail-sitter UAV 160 has fixed wings 162 to provide lift andallow the UAV 160 to glide horizontally (e.g., along the x-axis, in aposition that is approximately perpendicular to the position shown inFIG. 1D). However, the fixed wings 162 also allow the tail-sitter UAV160 to take off and land vertically on its own.

For example, at a launch site, the tail-sitter UAV 160 may be positionedvertically (as shown) with its fins 164 and/or wings 162 resting on theground and stabilizing the UAV 160 in the vertical position. Thetail-sitter UAV 160 may then take off by operating its propellers 166 togenerate an upward thrust (e.g., a thrust that is generally along they-axis). Once at a suitable altitude, the tail-sitter UAV 160 may useits flaps 168 to reorient itself in a horizontal position, such that itsfuselage 170 is closer to being aligned with the x-axis than the y-axis.Positioned horizontally, the propellers 166 may provide forward thrustso that the tail-sitter UAV 160 can fly in a similar manner as a typicalairplane.

Many variations on the illustrated fixed-wing UAVs are possible. Forinstance, fixed-wing UAVs may include more or fewer propellers, and/ormay utilize a ducted fan or multiple ducted fans for propulsion.Further, UAVs with more wings (e.g., an “x-wing” configuration with fourwings), with fewer wings, or even with no wings, are also possible.

As noted above, some embodiments may involve other types of UAVs, inaddition to or in the alternative to fixed-wing UAVs. For instance, FIG.1E shows an example of a rotorcraft that is commonly referred to as amulticopter 180. The multicopter 180 may also be referred to as aquadcopter, as it includes four rotors 182. It should be understood thatexample embodiments may involve a rotorcraft with more or fewer rotorsthan the multicopter 180. For example, a helicopter typically has tworotors. Other examples with three or more rotors are possible as well.Herein, the term “multicopter” refers to any rotorcraft having more thantwo rotors, and the term “helicopter” refers to rotorcraft having tworotors.

Referring to the multicopter 180 in greater detail, the four rotors 182provide propulsion and maneuverability for the multicopter 180. Morespecifically, each rotor 182 includes blades that are attached to amotor 184. Configured as such, the rotors 182 may allow the multicopter180 to take off and land vertically, to maneuver in any direction,and/or to hover. Further, the pitch of the blades may be adjusted as agroup and/or differentially, and may allow the multicopter 180 tocontrol its pitch, roll, yaw, and/or altitude.

It should be understood that references herein to an “unmanned” aerialvehicle or UAV can apply equally to autonomous and semi-autonomousaerial vehicles. In an autonomous implementation, all functionality ofthe aerial vehicle is automated; e.g., pre-programmed or controlled viareal-time computer functionality that responds to input from varioussensors and/or pre-determined information. In a semi-autonomousimplementation, some functions of an aerial vehicle may be controlled bya human operator, while other functions are carried out autonomously.Further, in some embodiments, a UAV may be configured to allow a remoteoperator to take over functions that can otherwise be controlledautonomously by the UAV. Yet further, a given type of function may becontrolled remotely at one level of abstraction and performedautonomously at another level of abstraction. For example, a remoteoperator could control high level navigation decisions for a UAV, suchas by specifying that the UAV should travel from one location to another(e.g., from a warehouse in a suburban area to a delivery address in anearby city), while the UAV's navigation system autonomously controlsmore fine-grained navigation decisions, such as the specific route totake between the two locations, specific flight controls to achieve theroute and avoid obstacles while navigating the route, and so on.

More generally, it should be understood that the example UAVs describedherein are not intended to be limiting. Example embodiments may relateto, be implemented within, or take the form of any type of unmannedaerial vehicle.

III. ILLUSTRATIVE UAV COMPONENTS

FIG. 2 is a simplified block diagram illustrating components of a UAV200, according to an example embodiment. UAV 200 may take the form of,or be similar in form to, one of the UAVs 100, 120, 140, 160, and 180described in reference to FIGS. 1A-1E. However, UAV 200 may also takeother forms.

UAV 200 may include various types of sensors, and may include acomputing system configured to provide the functionality describedherein. In the illustrated embodiment, the sensors of UAV 200 include aninertial measurement unit (IMU) 202, ultrasonic sensor(s) 204, and a GPS206, among other possible sensors and sensing systems.

In the illustrated embodiment, UAV 200 also includes one or moreprocessors 208. A processor 208 may be a general-purpose processor or aspecial purpose processor (e.g., digital signal processors, applicationspecific integrated circuits, etc.). The one or more processors 208 canbe configured to execute computer-readable program instructions 212 thatare stored in the data storage 210 and are executable to provide thefunctionality of a UAV described herein.

The data storage 210 may include or take the form of one or morecomputer-readable storage media that can be read or accessed by at leastone processor 208. The one or more computer-readable storage media caninclude volatile and/or non-volatile storage components, such asoptical, magnetic, organic or other memory or disc storage, which can beintegrated in whole or in part with at least one of the one or moreprocessors 208. In some embodiments, the data storage 210 can beimplemented using a single physical device (e.g., one optical, magnetic,organic or other memory or disc storage unit), while in otherembodiments, the data storage 210 can be implemented using two or morephysical devices.

As noted, the data storage 210 can include computer-readable programinstructions 212 and perhaps additional data, such as diagnostic data ofthe UAV 200. As such, the data storage 210 may include programinstructions 212 to perform or facilitate some or all of the UAVfunctionality described herein. For instance, in the illustratedembodiment, program instructions 212 include a navigation module 214 anda tether control module 216.

A. Sensors

In an illustrative embodiment, IMU 202 may include both an accelerometerand a gyroscope, which may be used together to determine an orientationof the UAV 200. In particular, the accelerometer can measure theorientation of the vehicle with respect to earth, while the gyroscopemeasures the rate of rotation around an axis. IMUs are commerciallyavailable in low-cost, low-power packages. For instance, an IMU 202 maytake the form of or include a miniaturized MicroElectroMechanical System(MEMS) or a NanoElectroMechanical System (NEMS). Other types of IMUs mayalso be utilized.

An IMU 202 may include other sensors, in addition to accelerometers andgyroscopes, which may help to better determine position and/or help toincrease autonomy of the UAV 200. Two examples of such sensors aremagnetometers and pressure sensors. In some embodiments, a UAV mayinclude a low-power, digital 3-axis magnetometer, which can be used torealize an orientation independent electronic compass for accurateheading information. However, other types of magnetometers may beutilized as well. Other examples are also possible. Further, note that aUAV could include some or all of the above-described inertia sensors asseparate components from an IMU.

UAV 200 may also include a pressure sensor or barometer, which can beused to determine the altitude of the UAV 200. Alternatively, othersensors, such as sonic altimeters or radar altimeters, can be used toprovide an indication of altitude, which may help to improve theaccuracy of and/or prevent drift of an IMU.

In a further aspect, UAV 200 may include one or more sensors that allowthe UAV to sense objects in the environment. For instance, in theillustrated embodiment, UAV 200 includes ultrasonic sensor(s) 204.Ultrasonic sensor(s) 204 can determine the distance to an object bygenerating sound waves and determining the time interval betweentransmission of the wave and receiving the corresponding echo off anobject. A typical application of an ultrasonic sensor for unmannedvehicles or IMUs is low-level altitude control and obstacle avoidance.An ultrasonic sensor can also be used for vehicles that need to hover ata certain height or need to be capable of detecting obstacles. Othersystems can be used to determine, sense the presence of, and/ordetermine the distance to nearby objects, such as a light detection andranging (LIDAR) system, laser detection and ranging (LADAR) system,and/or an infrared or forward-looking infrared (FLIR) system, amongother possibilities.

In some embodiments, UAV 200 may also include one or more imagingsystem(s). For example, one or more still and/or video cameras may beutilized by UAV 200 to capture image data from the UAV's environment. Asa specific example, charge-coupled device (CCD) cameras or complementarymetal-oxide-semiconductor (CMOS) cameras can be used with unmannedvehicles. Such imaging sensor(s) have numerous possible applications,such as obstacle avoidance, localization techniques, ground tracking formore accurate navigation (e.g., by applying optical flow techniques toimages), video feedback, and/or image recognition and processing, amongother possibilities.

UAV 200 may also include a GPS receiver 206. The GPS receiver 206 may beconfigured to provide data that is typical of well-known GPS systems,such as the GPS coordinates of the UAV 200. Such GPS data may beutilized by the UAV 200 for various functions. As such, the UAV may useits GPS receiver 206 to help navigate to the caller's location, asindicated, at least in part, by the GPS coordinates provided by theirmobile device. Other examples are also possible.

B. Navigation and Location Determination

The navigation module 214 may provide functionality that allows the UAV200 to, e.g., move about its environment and reach a desired location.To do so, the navigation module 214 may control the altitude and/ordirection of flight by controlling the mechanical features of the UAVthat affect flight (e.g., its rudder(s), elevator(s), aileron(s), and/orthe speed of its propeller(s)).

In order to navigate the UAV 200 to a target location (e.g., a deliverylocation), the navigation module 214 may implement various navigationtechniques, such as map-based navigation and localization-basednavigation, for instance. With map-based navigation, the UAV 200 may beprovided with a map of its environment, which may then be used tonavigate to a particular location on the map. With localization-basednavigation, the UAV 200 may be capable of navigating in an unknownenvironment using localization. Localization-based navigation mayinvolve the UAV 200 building its own map of its environment andcalculating its position within the map and/or the position of objectsin the environment. For example, as a UAV 200 moves throughout itsenvironment, the UAV 200 may continuously use localization to update itsmap of the environment. This continuous mapping process may be referredto as simultaneous localization and mapping (SLAM). Other navigationtechniques may also be utilized.

In some embodiments, the navigation module 214 may navigate using atechnique that relies on waypoints. In particular, waypoints are sets ofcoordinates that identify points in physical space. For instance, anair-navigation waypoint may be defined by a certain latitude, longitude,and altitude. Accordingly, navigation module 214 may cause UAV 200 tomove from waypoint to waypoint, in order to ultimately travel to a finaldestination (e.g., a final waypoint in a sequence of waypoints).

In a further aspect, the navigation module 214 and/or other componentsand systems of the UAV 200 may be configured for “localization” to moreprecisely navigate to the scene of a target location. More specifically,it may be desirable in certain situations for a UAV to be within athreshold distance of the target location where a payload 228 is beingdelivered by a UAV (e.g., within a few feet of the target destination).To this end, a UAV may use a two-tiered approach in which it uses amore-general location-determination technique to navigate to a generalarea that is associated with the target location, and then use amore-refined location-determination technique to identify and/ornavigate to the target location within the general area.

For example, the UAV 200 may navigate to the general area of a targetdestination where a payload 228 is being delivered using waypointsand/or map-based navigation. The UAV may then switch to a mode in whichit utilizes a localization process to locate and travel to a morespecific location. For instance, if the UAV 200 is to deliver a payloadto a user's home, the UAV 200 may need to be substantially close to thetarget location in order to avoid delivery of the payload to undesiredareas (e.g., onto a roof, into a pool, onto a neighbor's property,etc.). However, a GPS signal may only get the UAV 200 so far (e.g.,within a block of the user's home). A more preciselocation-determination technique may then be used to find the specifictarget location.

Various types of location-determination techniques may be used toaccomplish localization of the target delivery location once the UAV 200has navigated to the general area of the target delivery location. Forinstance, the UAV 200 may be equipped with one or more sensory systems,such as, for example, ultrasonic sensors 204, infrared sensors (notshown), and/or other sensors, which may provide input that thenavigation module 214 utilizes to navigate autonomously orsemi-autonomously to the specific target location.

As another example, once the UAV 200 reaches the general area of thetarget delivery location (or of a moving subject such as a person ortheir mobile device), the UAV 200 may switch to a “fly-by-wire” modewhere it is controlled, at least in part, by a remote operator, who cannavigate the UAV 200 to the specific target location. To this end,sensory data from the UAV 200 may be sent to the remote operator toassist them in navigating the UAV 200 to the specific location.

As yet another example, the UAV 200 may include a module that is able tosignal to a passer-by for assistance in either reaching the specifictarget delivery location; for example, the UAV 200 may display a visualmessage requesting such assistance in a graphic display, play an audiomessage or tone through speakers to indicate the need for suchassistance, among other possibilities. Such a visual or audio messagemight indicate that assistance is needed in delivering the UAV 200 to aparticular person or a particular location, and might provideinformation to assist the passer-by in delivering the UAV 200 to theperson or location (e.g., a description or picture of the person orlocation, and/or the person or location's name), among otherpossibilities. Such a feature can be useful in a scenario in which theUAV is unable to use sensory functions or another location-determinationtechnique to reach the specific target location. However, this featureis not limited to such scenarios.

In some embodiments, once the UAV 200 arrives at the general area of atarget delivery location, the UAV 200 may utilize a beacon from a user'sremote device (e.g., the user's mobile phone) to locate the person. Sucha beacon may take various forms. As an example, consider the scenariowhere a remote device, such as the mobile phone of a person whorequested a UAV delivery, is able to send out directional signals (e.g.,via an RF signal, a light signal and/or an audio signal). In thisscenario, the UAV 200 may be configured to navigate by “sourcing” suchdirectional signals—in other words, by determining where the signal isstrongest and navigating accordingly. As another example, a mobiledevice can emit a frequency, either in the human range or outside thehuman range, and the UAV 200 can listen for that frequency and navigateaccordingly. As a related example, if the UAV 200 is listening forspoken commands, then the UAV 200 could utilize spoken statements, suchas “I'm over here!” to source the specific location of the personrequesting delivery of a payload.

In an alternative arrangement, a navigation module may be implemented ata remote computing device, which communicates wirelessly with the UAV200. The remote computing device may receive data indicating theoperational state of the UAV 200, sensor data from the UAV 200 thatallows it to assess the environmental conditions being experienced bythe UAV 200, and/or location information for the UAV 200. Provided withsuch information, the remote computing device may determine altitudinaland/or directional adjustments that should be made by the UAV 200 and/ormay determine how the UAV 200 should adjust its mechanical features(e.g., its rudder(s), elevator(s), aileron(s), and/or the speed of itspropeller(s)) in order to effectuate such movements. The remotecomputing system may then communicate such adjustments to the UAV 200 soit can move in the determined manner.

C. Communication Systems

In a further aspect, the UAV 200 includes one or more communicationsystems 218. The communications systems 218 may include one or morewireless interfaces and/or one or more wireline interfaces, which allowthe UAV 200 to communicate via one or more networks. Such wirelessinterfaces may provide for communication under one or more wirelesscommunication protocols, such as Bluetooth, WiFi (e.g., an IEEE 802.11protocol), Long-Term Evolution (LTE), WiMAX (e.g., an IEEE 802.16standard), a radio-frequency ID (RFID) protocol, near-fieldcommunication (NFC), and/or other wireless communication protocols. Suchwireline interfaces may include an Ethernet interface, a UniversalSerial Bus (USB) interface, or similar interface to communicate via awire, a twisted pair of wires, a coaxial cable, an optical link, afiber-optic link, or other physical connection to a wireline network.

In some embodiments, a UAV 200 may include communication systems 218that allow for both short-range communication and long-rangecommunication. For example, the UAV 200 may be configured forshort-range communications using Bluetooth and for long-rangecommunications under a CDMA protocol. In such an embodiment, the UAV 200may be configured to function as a “hot spot;” or in other words, as agateway or proxy between a remote support device and one or more datanetworks, such as a cellular network and/or the Internet. Configured assuch, the UAV 200 may facilitate data communications that the remotesupport device would otherwise be unable to perform by itself.

For example, the UAV 200 may provide a WiFi connection to a remotedevice, and serve as a proxy or gateway to a cellular service provider'sdata network, which the UAV might connect to under an LTE or a 3Gprotocol, for instance. The UAV 200 could also serve as a proxy orgateway to a high-altitude balloon network, a satellite network, or acombination of these networks, among others, which a remote device mightnot be able to otherwise access.

D. Power Systems

In a further aspect, the UAV 200 may include power system(s) 220. Thepower system 220 may include one or more batteries for providing powerto the UAV 200. In one example, the one or more batteries may berechargeable and each battery may be recharged via a wired connectionbetween the battery and a power supply and/or via a wireless chargingsystem, such as an inductive charging system that applies an externaltime-varying magnetic field to an internal battery.

In a further aspect, the power systems 220 of UAV 200 a power interfacefor electronically coupling to an external AC power source, and an AC/DCconverter coupled to the power interface and operable to convertalternating current to direct current that charges the UAV's battery orbatteries. For instance, the power interface may include a power jack orother electric coupling for connecting to a 110V, 120V, 220V, or 240V ACpower source. Such a power system may facilitate a recipient-assistedrecharging process, where a recipient can connect the UAV to a standardpower source at a delivery location, such as the recipient's home oroffice. Additionally or alternatively, power systems 220 could includean inductive charging interface, such that recipient-assisted rechargingcan be accomplished wirelessly via an inductive charging systeminstalled or otherwise available at the delivery location.

E. Payload Delivery

The UAV 200 may employ various systems and configurations in order totransport and deliver a payload 228. In some implementations, thepayload 228 of a given UAV 200 may include or take the form of a“package” designed to transport various goods to a target deliverylocation. For example, the UAV 200 can include a compartment, in whichan item or items may be transported. Such a package may one or more fooditems, purchased goods, medical items, or any other object(s) having asize and weight suitable to be transported between two locations by theUAV. In some embodiments, a payload 228 may simply be the one or moreitems that are being delivered (e.g., without any package housing theitems). And, in some embodiments, the items being delivered, thecontainer or package in which the items are transported, and/or othercomponents may all be considered to be part of the payload.

In some embodiments, the payload 228 may be attached to the UAV andlocated substantially outside of the UAV during some or all of a flightby the UAV. For example, the package may be tethered or otherwisereleasably attached below the UAV during flight to a target location. Inan embodiment where a package carries goods below the UAV, the packagemay include various features that protect its contents from theenvironment, reduce aerodynamic drag on the system, and prevent thecontents of the package from shifting during UAV flight.

For instance, when the payload 228 takes the form of a package fortransporting items, the package may include an outer shell constructedof water-resistant cardboard, plastic, or any other lightweight andwater-resistant material. Further, in order to reduce drag, the packagemay feature smooth surfaces with a pointed front that reduces thefrontal cross-sectional area. Further, the sides of the package maytaper from a wide bottom to a narrow top, which allows the package toserve as a narrow pylon that reduces interference effects on the wing(s)of the UAV. This may move some of the frontal area and volume of thepackage away from the wing(s) of the UAV, thereby preventing thereduction of lift on the wing(s) cause by the package. Yet further, insome embodiments, the outer shell of the package may be constructed froma single sheet of material in order to reduce air gaps or extramaterial, both of which may increase drag on the system. Additionally oralternatively, the package may include a stabilizer to dampen packageflutter. This reduction in flutter may allow the package to have a lessrigid connection to the UAV and may cause the contents of the package toshift less during flight.

In order to deliver the payload, the UAV may include a tether system221, which may be controlled by the tether control module 216 in orderto lower the payload 228 to the ground while the UAV hovers above. Thetether system 221 may include a tether, which is couplable to a payload228 (e.g., a package). The tether 224 may be wound on a spool that iscoupled to a motor 222 of the UAV (although passive implementations,without a motor, are also possible). The motor may be a DC motor (e.g.,a servo motor) that can be actively controlled by a speed controller,although other motor configurations are possible. In some embodiments,the tether control module 216 can control the speed controller to causethe 222 to rotate the spool, thereby unwinding or retracting the tetherand lowering or raising the payload coupling apparatus. In practice, aspeed controller may output a desired operating rate (e.g., a desiredRPM) for the spool, which may correspond to the speed at which thetether system should lower the payload towards the ground. The motor maythen rotate the spool so that it maintains the desired operating rate(or within some allowable range of operating rates).

In order to control the motor via a speed controller, the tether controlmodule 216 may receive data from a speed sensor (e.g., an encoder)configured to convert a mechanical position to a representative analogor digital signal. In particular, the speed sensor may include a rotaryencoder that may provide information related to rotary position (and/orrotary movement) of a shaft of the motor or the spool coupled to themotor, among other possibilities. Moreover, the speed sensor may takethe form of an absolute encoder and/or an incremental encoder, amongothers. So in an example implementation, as the motor causes rotation ofthe spool, a rotary encoder may be used to measure this rotation. Indoing so, the rotary encoder may be used to convert a rotary position toan analog or digital electronic signal used by the tether control module216 to determine the amount of rotation of the spool from a fixedreference angle and/or to an analog or digital electronic signal that isrepresentative of a new rotary position, among other options. Otherexamples are also possible.

In some embodiments, a payload coupling component (e.g., a hook oranother type of coupling component) can be configured to secure thepayload 228 while being lowered from the UAV by the tether. The couplingapparatus or component and can be further configured to release thepayload 228 upon reaching ground level via electrical orelectro-mechanical features of the coupling component. The payloadcoupling component can then be retracted to the UAV by reeling in thetether using the motor.

In some implementations, the payload 228 may be passively released onceit is lowered to the ground. For example, a payload coupling componentmay provide a passive release mechanism, such as one or more swing armsadapted to retract into and extend from a housing. An extended swing armmay form a hook on which the payload 228 may be attached. Upon loweringthe release mechanism and the payload 228 to the ground via a tether, agravitational force as well as a downward inertial force on the releasemechanism may cause the payload 228 to detach from the hook allowing therelease mechanism to be raised upwards toward the UAV. The releasemechanism may further include a spring mechanism that biases the swingarm to retract into the housing when there are no other external forceson the swing arm. For instance, a spring may exert a force on the swingarm that pushes or pulls the swing arm toward the housing such that theswing arm retracts into the housing once the weight of the payload 228no longer forces the swing arm to extend from the housing. Retractingthe swing arm into the housing may reduce the likelihood of the releasemechanism snagging the payload 228 or other nearby objects when raisingthe release mechanism toward the UAV upon delivery of the payload 228.

In another implementation, a payload coupling component may include ahook feature that passively releases the payload when the payloadcontacts the ground. For example, the payload coupling component maytake the form of or include a hook feature that is sized and shaped tointeract with a corresponding attachment feature (e.g., a handle orhole) on a payload taking the form of a container or tote. The hook maybe inserted into the handle or hole of the payload container, such thatthe weight of the payload keeps the payload container secured to thehook feature during flight. However, the hook feature and payloadcontainer may be designed such that when the container contacts theground and is supported from below, the hook feature slides out of thecontainer's attachment feature, thereby passively releasing the payloadcontainer. Other passive release configurations are also possible.

Active payload release mechanisms are also possible. For example,sensors such as a barometric pressure based altimeter and/oraccelerometers may help to detect the position of the release mechanism(and the payload) relative to the ground. Data from the sensors can becommunicated back to the UAV and/or a control system over a wirelesslink and used to help in determining when the release mechanism hasreached ground level (e.g., by detecting a measurement with theaccelerometer that is characteristic of ground impact). In otherexamples, the UAV may determine that the payload has reached the groundbased on a weight sensor detecting a threshold low downward force on thetether and/or based on a threshold low measurement of power drawn by thewinch when lowering the payload.

Other systems and techniques for delivering a payload, in addition or inthe alternative to a tethered delivery system are also possible. Forexample, a UAV 200 could include an air-bag drop system or a parachutedrop system. Alternatively, a UAV 200 carrying a payload could simplyland on the ground at a delivery location. Other examples are alsopossible.

In some arrangements, a UAV may not include a tether system 221. Forexample, a UAV could include an internal compartment or bay in which theUAV could hold items during transport. Such a compartment could beconfigured as a top-loading, side-loading, and/or bottom-loadingchamber. The UAV may include electrical and/or mechanical means (e.g.,doors) that allow the interior compartment in the UAV to be opened andclosed. Accordingly, the UAV may open the compartment in variouscircumstances, such as: (a) when picking up an item for delivery at anitem source location, such that the item can be placed in the UAV fordelivery, (b) upon arriving at a delivery location, such that therecipient can place an item for return into the UAV, and/or (c) in othercircumstances. Further, it is also contemplated, that other non-tetheredmechanisms for securing payload items to a UAV are also possible, suchas various fasteners for securing items to the UAV housing, among otherpossibilities. Yet further, a UAV may include an internal compartmentfor transporting items and/or other non-tethered mechanisms for securingpayload items, in addition or in the alternative to a tether system 221.

F. Package Identification Device

The UAV 200 can include a package identification device 230 that can beused to identify payload 228. Within examples, the packageidentification device 230 can be arranged on a surface of the UAV 200that has a direct view of the payload 228. For instance, the packageidentification device 230 can be arranged on a surface of a payloadcompartment (see, e.g., compartments 506 and 604 in FIGS. 5 and 6,respectively). Other arrangements are possible.

Within examples, the package identification device 230 can be a sensoror a scanner that employs various technologies to interact with thepayload 228 in order to identify the payload 228. For instance, thepackage identification device 230 can employ one or more wirelesscommunication protocols, such as Bluetooth, WiFi (e.g., an IEEE 802.11protocol), Long-Term Evolution (LTE), WiMAX (e.g., an IEEE 802.16standard), a radio-frequency ID (RFID) protocol, near-fieldcommunication (NFC), and/or other wireless communication protocols.Additionally and/or alternatively, the package identification device 230can employ various scanning technologies such as a 1-D or 2-D barcodescanner. Additionally and/or alternatively, the package identificationdevice 230 can employ various image-capturing technologies such ascameras. Additionally and/or alternatively, the package identificationdevice 230 can employ various text recognition software that can readidentifying text (e.g., printed or handwritten) on the package.

IV. ILLUSTRATIVE UAV DEPLOYMENT SYSTEMS

UAV systems may be implemented in order to provide various UAV-relatedservices. In particular, UAVs may be provided at a number of differentlaunch sites that may be in communication with regional and/or centralcontrol systems. Such a distributed UAV system may allow UAVs to bequickly deployed to provide services across a large geographic area(e.g., that is much larger than the flight range of any single UAV). Forexample, UAVs capable of carrying payloads may be distributed at anumber of launch sites across a large geographic area (possibly eventhroughout an entire country, or even worldwide), in order to provideon-demand transport of various items to locations throughout thegeographic area. FIG. 3 is a simplified block diagram illustrating adistributed UAV system 300, according to an example embodiment.

In the illustrative UAV system 300, an access system 302 may allow forinteraction with, control of, and/or utilization of a network of UAVs304. In some embodiments, an access system 302 may be a computing systemthat allows for human-controlled dispatch of UAVs 304. As such, thecontrol system may include or otherwise provide a user interface throughwhich a user can access and/or control the UAVs 304.

In some embodiments, dispatch of the UAVs 304 may additionally oralternatively be accomplished via one or more automated processes. Forinstance, the access system 302 may dispatch one of the UAVs 304 totransport a payload to a target location, and the UAV may autonomouslynavigate to the target location by utilizing various on-board sensors,such as a GPS receiver and/or other various navigational sensors.

Further, the access system 302 may provide for remote operation of aUAV. For instance, the access system 302 may allow an operator tocontrol the flight of a UAV via its user interface. As a specificexample, an operator may use the access system 302 to dispatch a UAV 304to a target location. The UAV 304 may then autonomously navigate to thegeneral area of the target location. At this point, the operator may usethe access system 302 to take control of the UAV 304 and navigate theUAV to the target location (e.g., to a particular person to whom apayload is being transported). Other examples of remote operation of aUAV are also possible.

In an illustrative embodiment, the UAVs 304 may take various forms. Forexample, each of the UAVs 304 may be a UAV such as those illustrated inFIG. 1, 2, 3, or 4. However, UAV system 300 may also utilize other typesof UAVs without departing from the scope of the invention. In someimplementations, all of the UAVs 304 may be of the same or a similarconfiguration. However, in other implementations, the UAVs 304 mayinclude a number of different types of UAVs. For instance, the UAVs 304may include a number of types of UAVs, with each type of UAV beingconfigured for a different type or types of payload deliverycapabilities.

The UAV system 300 may further include a remote device 306, which maytake various forms. Generally, the remote device 306 may be any devicethrough which a direct or indirect request to dispatch a UAV can bemade. (Note that an indirect request may involve any communication thatmay be responded to by dispatching a UAV, such as requesting a packagedelivery). In an example embodiment, the remote device 306 may be amobile phone, tablet computer, laptop computer, personal computer, orany network-connected computing device. Further, in some instances, theremote device 306 may not be a computing device. As an example, astandard telephone, which allows for communication via plain oldtelephone service (POTS), may serve as the remote device 306. Othertypes of remote devices are also possible.

Further, the remote device 306 may be configured to communicate withaccess system 302 via one or more types of communication network(s) 308.For example, the remote device 306 may communicate with the accesssystem 302 (or a human operator of the access system 302) bycommunicating over a POTS network, a cellular network, and/or a datanetwork such as the Internet. Other types of networks may also beutilized.

In some embodiments, the remote device 306 may be configured to allow auser to request pick-up of one or more items from a certain sourcelocation and/or delivery of one or more items to a desired location. Forexample, a user could request UAV delivery of a package to their homevia their mobile phone, tablet, or laptop. As another example, a usercould request dynamic delivery to wherever they are located at the timeof delivery. To provide such dynamic delivery, the UAV system 300 mayreceive location information (e.g., GPS coordinates, etc.) from theuser's mobile phone, or any other device on the user's person, such thata UAV can navigate to the user's location (as indicated by their mobilephone).

In some embodiments, a business user (e.g., a restaurant) could utilizeone or more remote devices 306 to request that a UAV be dispatched topick-up one or more items (e.g., a food order) from a source location(e.g., the restaurant's address), and then deliver the one or more itemsto a target location (e.g., a customer's address). Further, in suchembodiments, there may be a number of remote devices 306 associated witha common item-provider account (e.g., an account used by multipleemployees and/or owners of a particular restaurant). Additionally, insuch embodiments, a remote device 306 may be utilized to senditem-provider submissions to a transport-provider computing system(e.g., central dispatch system 310 and or local dispatch system 312),which each indicate a respective quantitative measure for a given amountof UAV transport service at a given future time. For example, remotedevice 306 may be utilized to generate and send an item-providersubmission that specifies a level of desired UAV transport services(e.g., number and/or rate of expected UAV delivery flights), and/or amonetary value corresponding to the item provider's need for UAVtransport services, at a particular time or during a particular periodof time in the future.

In an illustrative arrangement, the central dispatch system 310 may be aserver or group of servers, which is configured to receive dispatchmessages requests and/or dispatch instructions from the access system302. Such dispatch messages may request or instruct the central dispatchsystem 310 to coordinate the deployment of UAVs to various targetlocations. The central dispatch system 310 may be further configured toroute such requests or instructions to one or more local dispatchsystems 312. To provide such functionality, the central dispatch system310 may communicate with the access system 302 via a data network, suchas the Internet or a private network that is established forcommunications between access systems and automated dispatch systems.

In the illustrated configuration, the central dispatch system 310 may beconfigured to coordinate the dispatch of UAVs 304 from a number ofdifferent local dispatch systems 312. As such, the central dispatchsystem 310 may keep track of which UAVs 304 are located at which localdispatch systems 312, which UAVs 304 are currently available fordeployment, and/or which services or operations each of the UAVs 304 isconfigured for (in the event that a UAV fleet includes multiple types ofUAVs configured for different services and/or operations). Additionallyor alternatively, each local dispatch system 312 may be configured totrack which of its associated UAVs 304 are currently available fordeployment and/or are currently in the midst of item transport.

In some cases, when the central dispatch system 310 receives a requestfor UAV-related service (e.g., transport of an item) from the accesssystem 302, the central dispatch system 310 may select a specific UAV304 to dispatch. The central dispatch system 310 may accordinglyinstruct the local dispatch system 312 that is associated with theselected UAV to dispatch the selected UAV. The local dispatch system 312may then operate its associated deployment system 314 to launch theselected UAV. In other cases, the central dispatch system 310 mayforward a request for a UAV-related service to a local dispatch system312 that is near the location where the support is requested and leavethe selection of a particular UAV 304 to the local dispatch system 312.

In an example configuration, the local dispatch system 312 may beimplemented as a computing system at the same location as the deploymentsystem(s) 314 that it controls. For example, the local dispatch system312 may be implemented by a computing system installed at a building,such as a warehouse, where the deployment system(s) 314 and UAV(s) 304that are associated with the particular local dispatch system 312 arealso located. In other embodiments, the local dispatch system 312 may beimplemented at a location that is remote to its associated deploymentsystem(s) 314 and UAV(s) 304.

Numerous variations on and alternatives to the illustrated configurationof the UAV system 300 are possible. For example, in some embodiments, auser of the remote device 306 could request delivery of a packagedirectly from the central dispatch system 310. To do so, an applicationmay be implemented on the remote device 306 that allows the user toprovide information regarding a requested delivery, and generate andsend a data message to request that the UAV system 300 provide thedelivery. In such an embodiment, the central dispatch system 310 mayinclude automated functionality to handle requests that are generated bysuch an application, evaluate such requests, and, if appropriate,coordinate with an appropriate local dispatch system 312 to deploy aUAV.

Further, some or all of the functionality that is attributed herein tothe central dispatch system 310, the local dispatch system(s) 312, theaccess system 302, and/or the deployment system(s) 314 may be combinedin a single system, implemented in a more complex system (e.g., havingmore layers of control), and/or redistributed among the central dispatchsystem 310, the local dispatch system(s) 312, the access system 302,and/or the deployment system(s) 314 in various ways.

Yet further, while each local dispatch system 312 is shown as having twoassociated deployment systems 314, a given local dispatch system 312 mayalternatively have more or fewer associated deployment systems 314.Similarly, while the central dispatch system 310 is shown as being incommunication with two local dispatch systems 312, the central dispatchsystem 310 may alternatively be in communication with more or fewerlocal dispatch systems 312.

In a further aspect, the deployment systems 314 may take various forms.In some implementations, some or all of the deployment systems 314 maybe a structure or system that passively facilitates a UAV taking offfrom a resting position to begin a flight. For example, some or all ofthe deployment systems 314 may take the form of a landing pad, a hangar,and/or a runway, among other possibilities. As such, a given deploymentsystem 314 may be arranged to facilitate deployment of one UAV 304 at atime, or deployment of multiple UAVs (e.g., a landing pad large enoughto be utilized by multiple UAVs concurrently).

Additionally or alternatively, some or all of deployment systems 314 maytake the form of or include systems for actively launching one or moreof the UAVs 304. Such launch systems may include features that providefor an automated UAV launch and/or features that allow for ahuman-assisted UAV launch. Further, a given deployment system 314 may beconfigured to launch one particular UAV 304, or to launch multiple UAVs304.

Note that deployment systems 314 may also be configured to passivelyfacilitate and/or actively assist a UAV when landing. For example, thesame landing pad could be used for take-off and landing. Additionally oralternatively, a deployment system could include a robotic arm operableto receive an incoming UAV. A deployment system 314 could also includeother structures and/or systems to assist and/or facilitate UAV landingprocesses. Further, structures and/or systems to assist and/orfacilitate UAV landing processes may be implemented as separatestructures and/or systems, so long as UAVs can move or be moved from alanding structure or system to a deployment system 314 forre-deployment.

The deployment systems 314 may further be configured to provideadditional functions, including for example, diagnostic-relatedfunctions such as verifying system functionality of the UAV, verifyingfunctionality of devices that are housed within a UAV (e.g., a payloaddelivery apparatus), and/or maintaining devices or other items that arehoused in the UAV (e.g., by monitoring a status of a payload such as itstemperature, weight, etc.).

In some embodiments, local dispatch systems 312 (along with theirrespective deployment system(s) 314 may be strategically distributedthroughout an area such as a city. For example, local dispatch systems312 may be strategically distributed such that each local dispatchsystems 312 is proximate to one or more payload pickup locations (e.g.,near a restaurant, store, or warehouse). However, the local dispatchsystems 312 may be distributed in other ways, depending upon theparticular implementation.

As an additional example, kiosks that allow users to transport packagesvia UAVs may be installed in various locations. Such kiosks may includeUAV launch systems, and may allow a user to provide their package forloading onto a UAV and pay for UAV shipping services, among otherpossibilities. Other examples are also possible.

In a further aspect, the UAV system 300 may include or have access to auser-account database 316. The user-account database 316 may includedata for a number of user accounts, and which are each associated withone or more person. For a given user account, the user-account database316 may include data related to or useful in providing UAV-relatedservices. Typically, the user data associated with each user account isoptionally provided by an associated user and/or is collected with theassociated user's permission.

Further, in some embodiments, a person may be required to register for auser account with the UAV system 300, if they wish to be provided withUAV-related services by the UAVs 304 from UAV system 300. As such, theuser-account database 316 may include authorization information for agiven user account (e.g., a user name and password), and/or otherinformation that may be used to authorize access to a user account.

In some embodiments, a person may associate one or more of their deviceswith their user account, such that they can access the services of UAVsystem 300. For example, when a person uses an associated mobile phoneto, e.g., place a call to an operator of the access system 302 or send amessage requesting a UAV-related service to a dispatch system, the phonemay be identified via a unique device identification number, and thecall or message may then be attributed to the associated user account.Other examples are also possible.

Additionally or alternatively, an item provider that wishes to delivertheir products using UAV transport services provided by an ATSP canregister for an item-provider account with the UAV system 300. As such,the user-account database 316 may include authorization information fora given item-provider account (e.g., one or more user name and passwordcombinations), and/or other information that may be used to authorizeaccess to a given item-provider account. Alternatively, data foritem-provider accounts may be kept in a separate database from recipientuser accounts. Other data structures and storage configurations forstoring such account data are also possible.

V. UAV TRANSPORT SERVICES WITH SEPARATELY LOCATED ITEM PROVIDERS AND UAVHUBS

As noted above, an ATSP can be a separate entity from the entity orentities that provide the items being transported and/or interface withthe recipients who request delivery of these items. For example, acompany that operates a fleet of UAVs configured for item delivery mayprovide delivery services for third-party entities, such as restaurants,clothing stores, grocery stores, and other “brick and mortar” and/oronline retailers, among other possibilities. These third-party entitiesmay have accounts with the UAV transport service provider, via which thethird-parties can request and/or purchase UAV transport services fromthe transport service provider. Further, the third-party entities couldinterface with recipients (e.g., customers) directly, or throughcomputing systems (e.g., applications and/or server systems) provided bythe UAV transport service provider.

FIG. 4 is a block diagram showing an example arrangement for an aerialtransport provider control system 402, which coordinates UAV transportservices for a plurality of item providers that are located remotelyfrom the service provider's dispatch locations, and served by aplurality of UAV hubs at various locations. As shown, an aerialtransport service provider (ATSP) 402 may be communicatively coupled toUAV nests 404 a to 404 d, and communicatively coupled to item-providercomputing systems 406 a to 406 d. Such communicative couplings may beimplemented using various types of wired and/or wireless communicationprotocols and networks.

Each UAV nest 404 a to 404 d is a facility where UAVs can be stored forat least a short period of time, and from which UAVs can begin carryingout a UAV transport task (e.g., where UAVs can take off). In someimplementations, some or all of UAV nests 404 a to 404 d may take theform of a local dispatch system and one or more deployment systems, suchas those described in reference to FIG. 3 above. Of course, some or allUAV nests 404 a to 404 d could also take other forms and/or performdifferent functions.

Each item-provider computing system 406 a to 406 d may be associatedwith a different item-provider account. As such, a given item-providercomputing system 406 a to 406 d may include one or more computingdevices that are authorized to access the corresponding item-provideraccount with ATSP 402. Further, ATSP 402 may store data foritem-provider accounts in an item-provider account database 407.

In practice, a given item-provider computing system 406 a to 406 d mayinclude one or more remote computing devices (e.g., such as one or moreremote devices 306 described in reference to FIG. 3), which have loggedin to or otherwise been authorized to access the same item-provideraccount (e.g., cell phones, laptops, and/or computing devices of abusiness's employees). Additionally or alternatively, an item-providercomputing system 406 a to 406 d may be implemented with less of anad-hoc approach; e.g., with one or more dedicated user-interfaceterminals installed at the item provider's facilities. Other types ofitem-provider computing systems are also possible.

In order to provide UAV transport services to various item providers inan efficient and flexible manner, a UAV transport service provider 402may dynamically assign different UAVs to transport tasks for differentitem providers based on demand and/or other factors, rather thanpermanently assigning each UAV to a particular item provider. As such,the particular UAV or UAVs that carry out transport tasks for a giventhird-party item provider may vary over time.

The dynamic assignment of UAVs to flights for a number of different itemproviders can help a UAV transport service provider to more efficientlyutilize a group of UAVs (e.g., by reducing unnecessary UAV downtime), ascompared to an arrangement where specific UAVs are permanently assignedto specific item providers. More specifically, to dynamically assignUAVs to transport requests from third-party item providers, the UAVtransport service provider 402 can dynamically redistribute UAVs amongsta number of UAV deployment locations (which may be referred to as, e.g.,“hubs” or “nests”) through a service area, according to time-varyinglevels of demand at various locations or sub-areas within the servicearea.

With such an arrangement, a delivery flight may involve the additionalflight leg to fly from the UAV hub to the item-provider's location topick up the item or items for transport, before flying to the deliverylocation, as compared to an arrangement where delivery UAVs arestationed at the source location for items (such as a distributor orretailer warehouse or a restaurant). While the flight leg between theUAV hub and a loading location has associated costs, these costs can beoffset by more efficient use of each UAV (e.g., more flights, and lessunnecessary ground time, in a given period of time), which in turn canallow for a lesser number of UAVs to be utilized for a given number oftransport tasks.

VI. METHODS FOR UPDATING A TRANSPORT TASK OF A UAV

As noted, some example embodiments can involve methods that can increasethe efficiency, reliability, and speed of the transportation servicesprovided by the ATSP. In an embodiment, a method can involve the ATSPdynamically updating a transport task of a UAV based on a package thatis picked up by the UAV. Doing so allows the UAV to receive a route to adelivery location of any item that the UAV picks up. As such, the UAVdoes not need to be assigned a specific item for pick up, and the UAVcan pick up any item that is ready for delivery without wasting itsresources waiting for the item provider to locate an item that isassigned to the UAV. Additionally, as explained herein, the capabilityof dynamically updating the transport task of the UAV based on thepackage picked up by the UAV can allow the ATSP to correct any detectederrors at an early stage in the delivery.

As explained above, the ATSP can provide transport services to an itemprovider in response to receiving a transport service request from theitem provider. The request can include information about the loadinglocation and information about the packages for delivery, such as aquantity, dimensions, delivery locations, and characteristics of thepackages, among other information. A package can include different typesof goods and items, typically sold by the item provider. In an example,the package can include one or more goods or items that are going to thesame delivery location.

In an embodiment, the ATSP can process the request to determine aquantity of UAVs to send to the loading location. In an example, theATSP can deploy a UAV for each delivery location provided in therequest. As such, packages that are being delivered to the same locationcan be delivered the same UAV. In other examples, the ATSP can deploymore than one UAV for each delivery location if the packages that are tobe delivered to the delivery location would not fit in a payloadcompartment of a single UAV. Then, to deploy the UAVs, the ATSP canassign each UAV a respective transport task that instructs the UAV tofly to the loading location to pick up one or more packages.

In line with the discussion above, to expedite the pick-up process, whena UAV arrives at a loading location, the transport task can instruct theUAV to pick up a package at random, in a predetermined order orsequence, or otherwise without specific package assignment, from thepackages that are ready for delivery at the loading location. In anexample, the UAVs can pick up packages in an order of arrival to theloading location. As such, the UAVs can avoid any potential collisionsthat could result from more than one UAV attempting to pick up the samepackage at the same time. In another example, the ATSP can assign theUAVs an order in which to pick up packages. Other examples ofdetermining an order in which the UAVs pick up packages are alsopossible.

In an embodiment, at the loading location, a package can be loaded bythe item provider into a payload compartment of the UAV. For instance,the item provider can use manual labor or automation (e.g., a roboticarm) to load packages into the payload compartment. The UAV can idle asthe package is being loaded until the UAV determines that the packagehas been secured in the payload compartment, perhaps using sensorslocated in the payload compartment. If the package is not secured in thepayload compartment, the UAV can provide the item provider with analert, such as a visual alert on a device that the item provider uses tointerface with the ATSP or an audible sound (e.g., an alarm).

Once the package is secured in the payload compartment, the package canbegin to depart the loading location. As the UAV is doing so, the ATSPcan identify the package in the payload compartment, perhaps using apackage identification device installed in the payload compartment. Inparticular, the package identification device can identify the packageby scanning, reading, or otherwise sensing a unique identifier coupledto the package. The unique identifier can be some combination of a 1-Dor 2-D barcode, RFID, printed label, or other identifying feature,attached to the package. Additionally and/or alternatively, the packagecan include electrical contacts that can couple with the packageidentification device, which allow the package to interface with thepackage identification device (and by extension the ATSP). Accordingly,the package identification device can include a scanner that can read1-D or 2-D barcodes or perform OCR on a printed label, an RFID reader, aBluetooth or Bluetooth Low Energy (BLE) module, and/or electricaloutlets that can couple to the electrical contacts on the package, amongother examples.

Once the package identification device determines the unique identifierof the package, the device can send the unique identifier to the ATSP.The ATSP can use the unique identifier to identify the package, forexample by searching the task requests sent to the ATSP by the itemprovider. Within examples, the transport task requests can includeinformation about the package, including a delivery location of thepackage, a dimension of the package, a scheduled time of delivery, alevel of urgency, fragility, a temperature constraint on the package,among other information. Accordingly, the ATSP can use the uniqueidentifier to determine, among other things, the delivery location ofthe package.

Once the ATSP determines the delivery location of the package, the ATSPcan generate a task update for the UAV. In particular, the task updatecan include a delivery location of package in the payload compartment ofthe UAV. For instance, the task update can include a route from acurrent location of the UAV (e.g., the loading location) to the deliverylocation. The task update can include other information about thedelivery location such as where to drop-off package at the deliverylocation, and whether there are additional delivery instructions for thepackage (e.g., required signature for receipt of the package). The UAVcan then proceed to the fly to the delivery location to deliver thepackage.

FIGS. 5A and 5B illustrate a UAV 500 arranged in accordance with thepresent disclosure. Although, the UAV 500 is shown as taking the form ofa quadcopter UAV, a UAV arranged in accordance with the presentdisclosure could take on any feasible form.

FIGS. 5A and 5B illustrate a top perspective in which a top side of theUAV 500 is shown. As shown, the UAV 500 includes a propulsion unit 502having unexposed propellers that are surrounded by a casing. Further,the UAV 500 includes a fuselage 504 to which the propulsion unit 502 isconnected. Yet further, the UAV 500 includes a payload compartment 506that is formed within the fuselage 504, thereby providing for loading ofa package into the compartment 506.

As illustrated in FIG. 5A, a package identification device 508 isarranged on an interior surface of the compartment 506. Within examples,the package identification device 508 can be one of: a scanner that canread 1-D or 2-D barcodes or perform OCR on a printed label, an RFIDreader, a Bluetooth or Bluetooth Low Energy (BLE) module, and/orelectrical outlets that can couple to electrical contacts on thepackage, among other examples. In some examples, more than one packageidentification device 508 can be installed in the compartment 508.Additionally and/or alternatively, the package identification device 508can be installed on any surface (interior or exterior) of thecompartment 506. Further, the package identification device 508 can beinstalled on any surface of the UAV 500. For instance, packageidentification device 508 can be arranged on an exterior surface of theUAV 500 such that a package may be identified as it is being loaded intothe UAV 500.

For example, as illustrated in FIG. 5B, the package identificationdevice 508 can be a scanner that emits beams 510 (visible or invisible)that can be used to read a unique identifier (e.g., unique identifier610 in FIG. 6) on a package that is loaded into the compartment 506. Insome examples, the unique identifier can be placed on a surface of thepackage. Accordingly, in order for the scanner 508 to be able to scanthe unique identifier, the surface with the unique identifier must befacing the scanner 508 when the package is placed into the compartment506. In such examples, to ensure that the package is placed in thecorrect orientation, the UAV 500 may include a visual indicator on thebody of the UAV indicating where the scanner 508 is located.Additionally and/or alternatively, the ATSP can inform the itemprovider, perhaps via computer device interface, where the scanner 508is located in the UAV 500.

In an embodiment, if the package identification device 508 does notdetect a unique identifier on a package, the UAV 500 can inform the ATSPthat the unique identifier is missing. In one example, the ATSP canidentify the package using a process of elimination (e.g., if all of theother packages to be picked up at a same location were identified, or byusing a weight, temperature range, or other identifying feature that maybe sensed by package identification device 508 or other sensors on UAV500). However, if the ATSP is not able to identify the package, thepackage can be returned to loading location or to a drop-off locationthat may be specified in advance or determined dynamically.

FIG. 6 illustrates a UAV 600 arranged in accordance with the presentdisclosure. As illustrated in FIG. 6, the UAV the compartment 604 isattached to the UAV 600 and located substantially outside of the UAV 600during some or all of a flight by the UAV 600. Specifically, thecompartment 604 is tethered or otherwise releasably attached below theUAV during flight to a delivery location. As also illustrated in FIG. 6,a package identifier device 606 is arranged on an interior surface ofthe compartment 600. In examples where the package identifier device 606is a scanner, the scanner 606 can scan a unique identifier (notillustrated) on a surface 608 of a package 602 that is being loaded intothe compartment 604. Within examples, a unique identifier may bearranged on more than one surface of the package 602. For instance, asillustrated in FIG. 6, in addition to the unique identifier (notillustrated) arranged on the surface 608, a unique identifier 610 isarranged on a surface 612 of the package. In other examples, compartment604 may be configured to have different (e.g., more aerodynamic) outershapes.

FIGS. 7A and 7B next illustrate scenarios in which the ATSP candynamically update a transport task of a UAV, according to exampleembodiments.

FIG. 7A illustrates scenario 700 in which an item provider requests fromthe ATSP to deliver packages 704A, 704B, 704C, and 704D, which arelocated at loading location 706 associated with the item provider. Inresponse to the request, the ATSP can assign transport tasks to UAVs702A, 702B, 702C, and 702D. In particular, the respective transport taskfor each UAV instructs the UAV to fly to the loading location 706, andto pick up a package from the packages 704A-704D. In an embodiment, thetransport tasks can instruct the UAVs 702A-702D to pick up packages inan order of arrival to the loading location 706. Additionally, thetransport task can instruct the UAVs to pick up packages at random.

Accordingly, the UAV 702A, which arrives first to the loading location706, can pick up a first package from the packages 704A-704D. Forinstance, the UAV 702A can randomly pick up the package 704A. Once thepackage 704A is loaded into a compartment of the UAV 704A, the UAV 704Aor the ATSP can inform the UAV that arrived after the UAV 704A that theUAV 704A has picked up a package. For instance, the UAV 704A can informthe UAV 704B, which arrived immediately after 702A, that the UAV 702Ahas picked up the package 704A.

Additionally, once the package 704A is loaded into a compartment of theUAV 704A, the ATSP can identify the package 704A. In particular, theATSP can use a package identification device located in the compartmentof the UAV 702A in order to identify the package 704A. For instance, thepackage identifier device can determine a unique identifier of thepackage, and can provide the unique identifier to the ATSP. The ATSP canthen use the unique identifier to determine information about thepackage 704A, perhaps by performing a search in a database provided bythe item provider. Other methods of determining information about thepackage are also possible.

In an embodiment, in response to identifying the package, the ATSP candetermine a route from the loading location 706 to a delivery locationof the package 704A. The ATSP can then update the transport task of theUAV 702A to provide the UAV 702A with the route so that the UAV 702A candeliver the package 704A by following the determined route. In anotherembodiment, the ATSP can determine a delivery location for each of theUAVs 702A-702D once all of the UAVs 702A-702D have picked up andidentified their respective packages. Based on the respective deliverylocation of each package, the ATSP can determine a respective route foreach of the UAVs 702A-702D. The ATSP can then send each of the UAVs702A-702D a respective task update that provides the respective UAV withthe respective route.

FIG. 7B illustrates a scenario 720 in which an item provider requestsfrom the ATSP to deliver packages 722A, 722B, 722C, and 722D. In thisscenario, the packages 722A-722D are each placed in a respective loadingpad 724A-724D. In this arrangement, the UAVs 702A-702D can each pick upa respective package simultaneously or within a short time period oftime with respect to one another. Other loading arrangements are alsopossible.

A. Detecting an Incorrect Package Loaded into the UAV

In some examples, it can still be useful to assign UAVs to pick upspecific packages, perhaps because of a special characteristic of apackage such as fragility. However, loading assigned packages into a UAVis error-prone. Specifically, when an item provider loads a package intoa payload compartment, it is possible, e.g., due to human error, thatthe item provider loads an incorrect package (i.e., a package that wasnot assigned to the UAV). In conventional practice, such errors oftenare not discovered until a later time, usually when the UAV delivers theincorrect package to a recipient that is supposed to receive the packagethat originally was assigned to the UAV. The recipient must then gothrough an extensive, and often cumbersome, process to return theincorrect package to the item provider and to receive the correctpackage. Not only that, but in instances where a delivery is timesensitive, a delivery mix-up will lead to an unsatisfactory customerexperience.

In an embodiment, the ATSP can avoid incorrect deliveries by updating atransport task of a UAV based on the package that is loaded into thepayload of the UAV. In particular, the ATSP can assign a transport taskto a UAV, where the transport task specifies a specific package to pickup and deliver. Additionally, the transport task can include a routefrom the UAV's starting location (e.g., a nest) to the loading location,and a route from the loading location to the delivery location of thespecific package. Accordingly, the UAV can follow the determined routefrom its starting position to the loading location to pick up anassigned package. At the loading location, an item provider can load apackage into a payload compartment of the UAV. Once the package issecured in a compartment payload, the UAV can begin to fly along theroute from the loading location to the delivery location of the UAV.

Additionally, once the package is secured in the payload compartment,the ATSP can identify the package in the compartment in order to confirmthat the package loaded into the payload compartment is indeed thepackage that is assigned to the UAV. For instance, the ATSP can cause apackage identification device to identify a unique identifier located onthe package. The ATSP can then use the unique identifier to determinewhether the package in the payload is the package that is assigned tothe UAV. If the package is in fact the package that is assigned to theUAV, the UAV can continue to fly to the delivery location of thepackage.

Conversely, if the package is not that package that is assigned to theUAV, then the ATSP can determine whether the UAV can deliver the“incorrect” package to its intended delivery location. For instance, theATSP can determine whether the UAV has enough battery power to completedelivery of the incorrect package to its intended delivery location, andin some cases, return to a nest or otherwise not become stranded. Inother examples, the ATSP also can consider further missions or transporttasks for the UAV in its determination of whether the UAV can completedelivery of said incorrect package. In still other examples, the ATSPalso can modify or adjust future missions or transport tasks for the UAVbased on dynamic updates being made to the current transport task. Ifthe UAV can deliver the package, then the ATSP can send a task update tothe UAV instructing the UAV to deliver the incorrect package.Additionally, the task update can include a route from a currentlocation of the UAV to a delivery location of the package. The ATSP canalso send assign a transport task to another UAV to pick up and deliverthe package

However, if the UAV is not capable of delivering the package, orinstructed to not deliver the package for any other reason, the UAV cansend a task update to the UAV instructing the UAV to return the packageto the loading location or another drop-off location. The ATSP can thenassign a transport task to another UAV instructing another UAV to pickup and deliver the package. Additionally, once the UAV returns or dropsoff the package, the ATSP can assign a transport task to the UAV to pickup and deliver the package that was supposed to be delivered initially.

Accordingly, by dynamically updating a transport task of a UAV based onthe package that is loaded into the UAV allows.

B. Example Methods of Operation

FIG. 8 is a flowchart illustrating a method 800, which relates todynamically updating a transport task of a UAV.

Method 800 shown in FIG. 8 (and other processes and methods disclosedherein) presents a method that can be implemented within an arrangementinvolving, for example, any of the systems shown in FIGS. 1A to 6 (ormore particularly by one or more components or subsystems thereof, suchas by a processor and a non-transitory computer-readable medium havinginstructions that are executable to cause the device to performfunctions described herein), among other possible systems.

Method 800 and other processes and methods disclosed herein may includeone or more operations, functions, or actions, as illustrated by one ormore of blocks 802-806 for instance. Although blocks are illustrated insequential order, these blocks may also be performed in parallel, and/orin a different order than those described herein. Also, the variousblocks may be combined into fewer blocks, divided into additionalblocks, and/or removed based upon the desired implementation.

In addition, for the method 800 and other processes and methodsdisclosed herein, the flowchart shows functionality and operation of onepossible implementation of the present disclosure. In this regard, eachblock may represent a module, a segment, or a portion of program code,which includes one or more instructions executable by a processor forimplementing specific logical functions or steps in the process. Theprogram code may be stored on any type of computer readable medium, forexample, such as a storage device including a disk or hard drive. Thecomputer readable medium may include non-transitory computer readablemedium, for example, such as computer-readable media that stores datafor short periods of time like register memory, processor cache andRandom Access Memory (RAM). The computer readable medium may alsoinclude non-transitory media, such as secondary or persistent long termstorage, like read only memory (ROM), optical or magnetic disks,compact-disc read only memory (CD-ROM), for example. The computerreadable media may also be any other volatile or non-volatile storagesystems. The computer readable medium may be considered a computerreadable storage medium, for example, or a tangible storage device. Inaddition, for the method 800 and other processes and methods disclosedherein, each block in FIG. 8 may represent circuitry that is wired toperform the specific logical functions in the process.

Within examples, the method 800 can be performed by an ATSP controlsystem, such as the ATSP control system 402 of FIG. 4. Alternatively,the method 800 can be performed by a controller of a UAV, e.g.,processor 208 of FIG. 2.

At block 802, the method 800 may involve receiving, at atransport-provider computing system, an item provider request fortransportation of a plurality of packages from a loading location at agiven future time. As explained above, an item provider (e.g., itemprovider 406 in FIG. 4A) could request from an ATSP control systemtransportation services for one or more packages. Within examples, eachpackage can include one or more items that are grouped together based onthe delivery destination of the items. For instance, items that aregrouped together in a package could be going to the same destination.Accordingly, the request can include information about the packages fordelivery such as quantity, dimensions and weight, delivery locations,urgency, fragility, among other examples.

At block 804, the method 800 may involve assigning a respectivetransport task to each of a plurality of unmanned aerial vehicles (UAV),wherein the respective transport task comprises an instruction to deployto the loading location to pick up one or more of the plurality ofpackages. In particular, a transport task for a UAV can instruct the UAVto fly to the loading location to pick up one or more of the pluralityof packages for delivery at the loading location. The transport task canalso include a route from a nest of the UAV to the loading location.This route is the first segment of the UAV's flight while performing thetask. In one example, the transport task does not assign the UAV aparticular package to pick up. As such, the generated task, at thispoint, only includes information about the first flight segment. Inanother example, the transport task does assign the UAV a particularpackage to pick up. Thus, the generated task can also include a routefor the second flight segment from the loading location to the deliverylocation of the particular package.

In response to receiving a transport task, each UAV can fly to theloading location. Once at the loading location, the plurality of UAVscan begin to pick up packages. In an example, if each of the pluralityof UAVs is not assigned particular packages, then each UAV can pick upany package as explained above. In another example, if each of theplurality of UAVs is assigned particular packages, then each UAV canpick up its assigned package.

At block 806, the method 800 may involve identifying a first packagewhile or after a first UAV of the plurality of UAVs picks up the firstpackage. During or after the first UAV picks up the first package andsecures the first package in a payload compartment of the UAV, a packageidentification device can identify the package, according to embodimentsdescribed herein. For instance, the package identification device canscan a label attached to the package in order to identify a uniqueidentifier located on the package.

At block 808, the method 800 may involve based on the identifying of thefirst package, providing a task update to the first UAV to update therespective transport task of the first UAV. In a first example, if thefirst UAV is not assigned a package, then the task update can update thetransport task to include a second flight segment. In particular, thesecond flight segment can be between the loading location and thedelivery location of the first package.

In a second example, if the first UAV is assigned a package, then thetask update can update the transport task if the first package is notthe package that is assigned to the first UAV. In this example, the taskupdate can instruct the UAV to deliver the first package to its intendedrecipient. Thus, the task update can update the delivery location of thetransport task from the delivery location of the particular package tothe delivery location of the first package that was loaded into thepayload compartment of the UAV. Alternatively, the task update caninstruct the UAV to drop-off the first package at a drop-off location orreturn it to the loading location.

FIG. 9 is a flowchart illustrating a method 900, which relates to a UAVreceiving a task update.

At block 902, the method 900 involves receiving a transport taskindicating an instruction to fly to a loading location to pick up apackage from a plurality of packages located at the loading location.For instance, the transport task can be received from an ATSP system. Atblock 904, the method 900 involves causing the UAV to fly to the loadinglocation. And at block 906, the method 900 involves at the loadinglocation, causing the UAV to pick up a first package from the pluralityof packages, which may be done at random, in a predetermined order orsequence, or otherwise without specific package assignment. At block908, the method involves causing the package identification device toscan, sense or otherwise interact with a unique identifier of the firstpackage. At block 910, the method involves communicating the uniqueidentifier to a transport-provider computing system (e.g., the ATSPsystem). At block 912, the method 900 involves receiving a task update.

III. CONCLUSION

While various aspects and embodiments have been disclosed herein, otheraspects and embodiments will be apparent to those skilled in the art.The various aspects and embodiments disclosed herein are for purposes ofillustration and are not intended to be limiting, with the true scopeand spirit being indicated by the following claims.

What is claimed is:
 1. A method comprising: receiving, at atransport-provider computing system, an item provider request fortransportation of a plurality of packages from a loading location at agiven future time; assigning, by the transport-provider computingsystem, a respective transport task to each of a plurality of unmannedaerial vehicles (UAV), wherein the respective transport task comprisesan instruction to deploy to the loading location to pick up one or moreof the plurality of packages; identifying, by the transport-providercomputing system, a first package while or after a first UAV of theplurality of UAVs picks up the first package; and based on theidentifying of the first package, providing, by the transport-providercomputing system, a task update to the first UAV to update therespective transport task of the first UAV.
 2. The method of claim 1,wherein a quantity of the plurality of UAVs is the same as a quantity ofthe plurality of packages.
 3. The method of claim 1, wherein theinstruction to deploy to the loading location to pick up one or morepackages comprises an instruction to pick up one package at random froma remaining set of the plurality of packages.
 4. The method of claim 3,wherein the instruction to pick up the one package further comprises aninstruction to pick up the one package in an order of arrival of the UAVto the loading location.
 5. The method of claim 1, wherein identifying,by the transport-provider computing system, a first package comprises:instructing, by the transport-provider computing system, a packageidentifying device installed within the payload compartment to identifythe first package.
 6. The method of claim 5, wherein scanning the firstpackage comprises scanning a label attached to the first package.
 7. Themethod of claim 1, wherein providing, by the transport-providercomputing system, a task update to the first UAV to update therespective transport task of the first UAV comprises: determining adelivery location of the first package; transmitting to the first UAV aroute from a current location of the UAV to the delivery location of thefirst package.
 8. The method of claim 1, wherein the method furthercomprises: identifying, by the transport-provider computing system, arespective package picked up by each UAV; and determining, by thetransport-provider computing system, a respective delivery location ofthe packages picked up the UAVs.
 9. The method of claim 8, wherein themethod further comprises: based on the respective delivery location ofthe respective package picked up by each UAV, determining, by thetransport-provider computing system, for each UAV a respective routefrom the loading location to the respective delivery location of therespective package picked up by the UAV.
 10. The method of claim 1,wherein the method further comprises: determining, by thetransport-provider computing system, that the respective transport taskfor the first UAV comprises an instruction to deliver a particularpackage; and determining, by the transport-provider computing system,that the first package is not the particular package.
 11. The method ofclaim 10, further comprising: determining, by the transport-providercomputing system, a first delivery location of the first package; andbased on one or more characteristics of the first UAV, determining, bythe transport-provider computing system, that the first UAV is capableof delivering the first package to the first delivery location.
 12. Themethod of claim 11, wherein the task update comprises an instruction todeliver the first package to the first delivery location.
 13. The methodof claim 10, wherein the task update is a first task update, and whereinthe method further comprises: determining, by the transport-providercomputing system, that a second UAV of the plurality is transporting theparticular package; and in response, providing, by thetransport-provider computing system, a second task update to the secondUAV to deliver the particular package to a delivery location of theparticular package.
 14. The method of claim 10, wherein the methodfurther comprises based on one or more characteristics of the first UAV,determining, by the transport-provider computing system, that the firstUAV is not capable of delivering the first package, and wherein the taskupdate comprises an instruction to drop off the first package at one of:the loading location and a nearby drop-off location.
 15. The method ofclaim 14, wherein the method further comprises: based on one or morecharacteristics of a second UAV, determining, by the transport-providercomputing system, that the second UAV is capable of delivering the firstpackage to a delivery location of the first package; and deploying, bythe transport-provider computing system, the second UAV to pick up thefirst package to deliver the first package to the delivery location ofthe first package.
 16. An unmanned aerial vehicle (UAV) comprising: apayload compartment operable to hold one or more packages; an itemidentification device arranged in an interior of the payloadcompartment, wherein the item identification device is configured toidentify the one or more packages held in the payload compartment; and acomputer apparatus having one or more processors and memory storinginstructions that, when executed by the one or more processors, causethe system to carry out operations including: receiving, from atransport-provider computing system, a transport task indicating aninstruction to fly to a loading location to pick up a package from aplurality of packages located at the loading location; causing the UAVto fly to the loading location; at the loading location, causing the UAVto pick up a first package from the plurality of packages; causing thepackage identification device to scan, sense or otherwise interact witha unique identifier of the first package; communicating the uniqueidentifier to the transport-provider computing system; and in response,receiving a task update from the transport-provider computing system.17. The unmanned aerial vehicle of claim 16, wherein the task update isindicative of at least one of: a delivery location of the first packageand a route to the delivery location of the first package.
 18. Theunmanned aerial vehicle of claim 16, wherein the transport task isfurther indicative of a particular package that the UAV is assigned topick up from the loading location.
 19. The unmanned aerial vehicle ofclaim 18, wherein the operations further comprise: determining that thefirst package is not the particular package, and wherein the task updateis indicative of an instruction to drop off the first package at adrop-off location.
 20. A non-transitory computer-readable medium havingstored thereon program instructions that when executed by the processorcause the computing device to perform a set of functions comprising:receiving an item provider request for transportation of a plurality ofpackages from a loading location at a given future time; assigning arespective transport task to each of a plurality of unmanned aerialvehicles (UAV), wherein the respective transport task comprises aninstruction to deploy to the loading location to pick up one or more ofthe plurality of packages; identifying a first package while or after afirst UAV of the plurality of UAVs picks up the first package; and basedon the identifying of the first package, providing a task update to thefirst UAV to update the respective transport task of the first UAV.